View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 64848U 26145.33845928 +.00000000 +00000-0 +29018-3 0 00006
2 64848 97.4480 0.7173 0001699 93.5084 266.6338 15.05656124 05
| Epoch (UTC): | 25 May 2026 08:07:22 |
| Eccentricity: | 0.0001699 |
| inclination: | 97.4480° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7173° |
| argument of perigee: | 93.5084° |
| revolutions per day: | 15.05656124 |
| mean anomaly at epoch: | 266.6338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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